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특허 상세정보

On-board flight control drag actuator system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/02    F42B-025/24   
미국특허분류(USC) 244/321 ; 102/384 ; 102/388 ; 244/328
출원번호 US-0669212 (1984-11-07)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 23  인용 특허 : 2
초록

A missile on-board flight pitch, yaw and roll control drag actuator system. The system having a plurality of control panels operated by an actuator drive. The actuator drive accurately positioning the panels in a desired position in the airstream of the missile for controlling the flight, orientation and speed of the aircraft.

대표
청구항

An on-board flight pitch, yaw and roll control drag actuator system for controlling the flight of a missile, the system comprising: a plurality of control panels hinged on the missile; an actuator connected to each pannel for opening and closing the panels into the airstream of the missile, the actuator connected to the panel using a two-way actuator drive with a gas operated piston mounted therein, the piston having an actutor rod extending outwardly therefrom, the end of the actuator rod connected to a slide lever attached to a hinged joint mounted at ...

이 특허를 인용한 특허 피인용횟수: 23

  1. Villaume, Fabrice. Active pitch control method and device for an aircraft. USP2010127853369.
  2. Rastegar, Jahangir S.; Spinelli, Thomas. Actuators for gun-fired projectiles and mortars. USP2015109151581.
  3. Rastegar, Jahangir S.; Spinelli, Thomas. Actuators for gun-fired projectiles and mortars. USP2011077973270.
  4. Clark,Walter Dennis. Aircraft with forward opening inlay spoilers for yaw control. USP2008117448578.
  5. Cannon James J. (Northridge CA) Elkanick Mark (Tucson AZ). Blended missile autopilot. USP1997015590850.
  6. Pettersson, Thomas. Brake panel for a detonator or a projectile. USP2017079702675.
  7. Lecat Robert J. (Centerport NY). Cable towed decoy with collapsible fins. USP1991075029773.
  8. Grosch, Hermann; Kaspari, Axel. Delivery system for a warhead with an orientation device for neutralizing mines. USP2003126662701.
  9. Schroeder Wayne K.. Dual-control scheme for improved missile maneuverability. USP200108RE37331.
  10. Schroeder Wayne K.. Method and apparatus for rapidly turning a vehicle in a fluid medium. USP2001106308911.
  11. Johnsson,Stig. Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith. USP2006097104497.
  12. Johnsson,Stig. Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith. USP2009027487934.
  13. Maynard, John A.; Carlson, Mark A.; Zemany, Paul D.. Optically guided munition control system and method. USP2013058450668.
  14. Baras, Christian; Spitzer, Denis; Comet, Marc; Ciszek, Fabrice; Sourgen, Frederic. Piloting device of a missile or of a projectile. USP2014058716640.
  15. Schleimann-Jensen Lars J. (182 34 Danderyd Ekbacksvagen SEX). Projectile steering apparatus and method. USP1990104966078.
  16. Kuhnle Joachim,DEX ; Heitmann Thomas,DEX ; Niemeyer Torsten,DEX ; Arendt Norbert,DEX. Projectile to be fired from a weapon barrel and stabilized by a guide assembly. USP2001116314886.
  17. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2012128338769.
  18. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2013128610042.
  19. Sankovic, John R.. Pyrotechnic fin deployment and retention mechanism. USP2012058183508.
  20. Schleimann-Jensen Lars J. (Ekbacksvgen 33A 182 34 Danderyd SEX). System for guiding a flying object towards a target. USP1990014890554.
  21. Teter, Roger D.; Kudlick, Dean A.; Williams, Richard M.. Three axis flap control system. USP2003016502785.
  22. Mark H. Yim. Tracking device. USP2002076422509.
  23. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.